Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer-Reference-Cited by-同舟云学术

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Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer

Published:2020-12 Issue:12 Volume:58 Page:5254-5263
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Xiong Youde¹,Yu Tao¹,Lin Liquan¹,Zhao Jiaquan¹,Wu Jie¹

Affiliation:

1. Huazhong University of Science and Technology, 430074 Wuhan, People’s Republic of China

Funder

National Numerical Wind-tunnel

National Natural Science Foundation of China

Research Funds for the Central Universities

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference53 articles.

1. Transition and Stability of High-Speed Boundary Layers

2. Boundary layer instability, transition and control

3. Hypersonic Stability and Transition Prediction

4. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies

5. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

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